GB853133A - Combustion chamber construction - Google Patents
Combustion chamber constructionInfo
- Publication number
- GB853133A GB853133A GB481858A GB481858A GB853133A GB 853133 A GB853133 A GB 853133A GB 481858 A GB481858 A GB 481858A GB 481858 A GB481858 A GB 481858A GB 853133 A GB853133 A GB 853133A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plate
- rib
- flank
- tube
- chamber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/68—Decomposition chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Catalysts (AREA)
Abstract
853,133. Generating combustion products under pressure; tube walls for furnaces. NAPIER & SON Ltd., D. Jan. 27, 1959 [Feb. 13, 1958], No. 4818/58. Class 51 (1). [Also in Groups XXVI and XXVIII] A combustion chamber 14, Fig. 1, of non-uniform crosssection is formed from a series of abutting flat tubes 17 of rectangular cross-section extending generally in the axial direction of the chamber and each comprising inner and outer plate-like members profiled along at least one flank to correspond with variations in the cross-section of the chamber along its axis, and two shallow flank elements at opposite edges of the tube, at least part of each flank element being formed as a rib adjacent the edge of and forming part of one of the plate-like members. The rib of each member is united as by welding to the edge or rib of the other plate-like member to form a fluid-tight tube and adjacent tubes are secured to one another along their flank edges. In Fig. 2, a platelike member 18 has a central rib 21 and edge ribs 19, 20 welded to a plate-like member in two parts 22, 23. In Fig. 4, the radially inner plate-like member 31 is of channel section and the outer member 32 is flat. In a further modification, both plate-like members are made of L-section plates. Each tube is bent to conform to the desired profile of the combustion chamber in a plane through the axis thereof. A coolant such as liquid hydrogen peroxide has access to the tubes through a gallery 28, Fig. 1, and leaves by a gallery 29 whence it passes through a passage 30 to the catalyst chamber 10 of a liquid-fuelled rocket motor.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB481858A GB853133A (en) | 1958-02-13 | 1958-02-13 | Combustion chamber construction |
| FR786117A FR1216110A (en) | 1958-02-13 | 1959-02-09 | Combustion chamber |
| DEN16259A DE1099805B (en) | 1958-02-13 | 1959-02-13 | Combustion chamber, especially for rocket engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB481858A GB853133A (en) | 1958-02-13 | 1958-02-13 | Combustion chamber construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB853133A true GB853133A (en) | 1960-11-02 |
Family
ID=9784378
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB481858A Expired GB853133A (en) | 1958-02-13 | 1958-02-13 | Combustion chamber construction |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1099805B (en) |
| FR (1) | FR1216110A (en) |
| GB (1) | GB853133A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110594036A (en) * | 2019-08-23 | 2019-12-20 | 西北工业大学 | Actively cooled dual-nozzle strut-plate ejection rocket for rocket-based combined-cycle engine |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3501916A (en) * | 1966-09-24 | 1970-03-24 | Bolkow Gmbh | Tubular components for forming a rocket engine combustion chamber |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH140212A (en) * | 1928-03-02 | 1930-05-31 | Holzwarth Hans Dr Ing E H | Combustion chamber. |
| NL30859C (en) * | 1930-09-02 | |||
| DE716175C (en) * | 1935-02-09 | 1942-01-14 | Eugen Saenger Dr Ing | Rocket engine |
-
1958
- 1958-02-13 GB GB481858A patent/GB853133A/en not_active Expired
-
1959
- 1959-02-09 FR FR786117A patent/FR1216110A/en not_active Expired
- 1959-02-13 DE DEN16259A patent/DE1099805B/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110594036A (en) * | 2019-08-23 | 2019-12-20 | 西北工业大学 | Actively cooled dual-nozzle strut-plate ejection rocket for rocket-based combined-cycle engine |
| CN110594036B (en) * | 2019-08-23 | 2020-06-02 | 西北工业大学 | Actively cooled dual-nozzle support plate ejector for rocket-based combined cycle engine |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1099805B (en) | 1961-02-16 |
| FR1216110A (en) | 1960-04-22 |
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